Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Dennis L. Tilley"'
Autor:
Dennis L. Tilley, Ronald A. Spores
Publikováno v:
Journal of Spacecraft and Rockets. 34:785-791
At typical Space Shuttle altitudes atmospheric drag is the dominant force limiting satellite on-orbit life (typically
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9b886925cdd73e6829813493c59ce82d
https://doi.org/10.2514/2.3287
https://doi.org/10.2514/2.3287
Publikováno v:
Journal of Propulsion and Power. 12:381-389
Theoretical studies indicate that a variety of microscopic and macroscopic plasma instabilities can significantly affect the performance of the magnetoplasmadynamic (MPD) thruster, yet experimental evidence for their existence is extremely limited. T
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f3a8cac73bba11ce203938ee1c586ea5
https://doi.org/10.2514/3.24040
https://doi.org/10.2514/3.24040
Publikováno v:
Review of Scientific Instruments. 65:678-681
The cylindrical triple probe method is an attractive technique for measuring electron temperatures (Te) and electron number densities (ne) in a variety of plasmas sources. In practice, however, the cylindrical triple probe can be sensitive to sources
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e4ef41d8c73d195983677b2838717d61
https://doi.org/10.1063/1.1145138
https://doi.org/10.1063/1.1145138
Publikováno v:
35th Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7ab1cb2610a2a52bc60e0c35d399c785
https://doi.org/10.2514/6.1999-2573
https://doi.org/10.2514/6.1999-2573
Publikováno v:
35th Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9eb8441abb2c9e4bfaeec5a4ee87d1a1
https://doi.org/10.2514/6.1999-2283
https://doi.org/10.2514/6.1999-2283
Publikováno v:
34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
The Primex Aerospace Company has developed a hollow cathode assembly (HCA) for Hall thruster applications. The technical basis for its design is the NASA HCA, which is flight qualified for the Space Station plasma contactor mission. The primary objec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f48ce5647175df16266ac716d8c12f47
https://doi.org/10.2514/6.1998-3339
https://doi.org/10.2514/6.1998-3339
The paper examines some of the benefits to gained in using Stationary Plasma Thruster (SPT) propulsion onboard small spacecraft. SPTs were developed in Russia, and have an extensive flight history, with over 70 thrusters flown since 1971. A joint ven
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1ee4c21bb6038c683d317591a9f77f30
https://doi.org/10.21236/ada437488
https://doi.org/10.21236/ada437488
Autor:
Salvador Castillo, Dennis L. Tilley
Publikováno v:
28th Joint Propulsion Conference and Exhibit.
The multi-megawatt, quasi-steady MPD thruster facility at the Air Force Phillips Laboratory is now fully operational. This operational status is the result of many modifications and improvements completed in the past year. An update of facility capab
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b1c398b22a8ea1b869e7fb96ec7329c7
https://doi.org/10.2514/6.1992-3158
https://doi.org/10.2514/6.1992-3158
Publikováno v:
21st International Electric Propulsion Conference.
The triple probe method is an attractive technique for measuring axial and radial profiles of electron temperature T(e) and electron number density n(e) in magnetoplasmadynamic (MPD) thruster plumes. In this paper the performance and applicability of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ad9b3c6554f43d80d959905b06cd3b0d
https://doi.org/10.2514/6.1990-2667
https://doi.org/10.2514/6.1990-2667